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The mariner 9 power subsystem design and flight performanceThe design and flight performance of the Mariner Mars 1971 power subsystem are presented. Mariner 9 was the first spacecraft to orbit another planet, and some of the power management techniques employed to support an orbital mission far from earth with marginal sunlight for its photovoltaic-battery power source are described. The performance of its nickel-cadmium battery during repetitive sun occultation phases of the mission, and the results of unique tests in flight to assess the performance capability of its solar array are reported.
Document ID
19730016369
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Josephs, R. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 7, 2013
Publication Date
May 15, 1973
Subject Category
Auxiliary Systems
Report/Patent Number
JPL-TM-33-616
NASA-CR-132992
Report Number: JPL-TM-33-616
Report Number: NASA-CR-132992
Accession Number
73N25096
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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